US5904287AExpiredUtility

Method of bonding graphite to metal

68
Assignee: NEC CORPPriority: Aug 13, 1993Filed: Jul 29, 1994Granted: May 18, 1999
Est. expiryAug 13, 2013(expired)· nominal 20-yr term from priority
C04B 2237/124C04B 2237/706C04B 2237/125C04B 2237/592C04B 37/026C04B 2237/403C04B 2237/127C04B 2237/708C23C 14/00B23K 35/005C04B 2237/407C04B 2235/6565C04B 2237/72C04B 37/025C23C 10/00C04B 2235/6562C04B 2237/88C04B 2237/363B23K 35/302C04B 2237/80C04B 2237/76C04B 2237/083C04B 2237/126C04B 2235/6581
68
PatentIndex Score
20
Cited by
12
References
5
Claims

Abstract

The method for bonding graphite to metal, includes the steps of forming a metal carbide layer on a surface of the graphite, the metal being to be bonded to said graphite, and brazing the graphite to the metal with an active alloy brazing material. The present invention is based on the fact discovered by the inventor that if a metal carbide layer is in advance formed on a surface of a graphite, an active metal such as Ti could more easily react on the metal carbide layer to thereby bond the metal to the graphite, rather than the case in which a graphite member is made to directly react on an active metal to thereby bond the graphite member to the metal.

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
       1. A method for bonding graphite to metal, comprising the steps of: forming a metal carbide layer having a thickness of at least 25 micrometers on a surface of said graphite, said metal carbide layer being composed of any one of metal carbides selected from the croup consisting of Tic TaC, ZrC and NbC; and   brazing said metal carbide layer to said metal with an active alloy brazing material to bond said graphite to said metal.   
     
     
       2. A method in accordance with claim 1, wherein said metal carbide layer has thickness in the range of 25 micrometers through 300 micrometers. 
     
     
       3. A method in accordance with claim 1, wherein said metal carbide layer is formed by chemical vapor reaction (CVR) process. 
     
     
       4. A method in accordance with claim 1, wherein said active alloy brazing material includes Ti. 
     
     
       5. A method in accordance with claim 1, wherein said graphite has thermal expansion coefficient which is different from that of said metal carbide layer by 1×10 -6  per degree or less.

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